FLIGHT CONTROL STICK REGULATOR AND FLIGHT CONTROLLER OF AIRPLANE HAVING AT LEAST ONE OF THE ABOVE REGULATOR

摘要

PURPOSE: To improve the controllability of an aircraft by supporting a tilting stick free to tilt in the longitudinal and lateral direction and free to rotate around an axis and transmitting electric signals in accordance with manipulated variable and rotational quantity in the longitudinal and lateral direction of this tilting stick respectively from each of different positional sensors. CONSTITUTION: These tilting sticks 20, 21 for an aircraft are tilted around a crossing axis X-X in the case when the aircraft pitches, oscillated around a major axis Y-Y in the case of restraining rolling and rotationally operated around an axis Z-Z in the case of restraining deflected pitching and rolling. Each of the tilting sticks 20, 21 is connected to a shaft 26 supported free to rotate in a fixed block 25 provided in a case 24 of each of systems 22, 23 by a universal joint 31 and an auxiliary axis 32. Additionally, it is devised so that an electric signal is transmitted from each of positional sensors 38-41 in accordance with movement of a sleeve 34 externally fitted in the auxiliary axis 32 and an integral cross member 37 and so that an electric signal is transmitted from each of positional sensors 50, 51 in accordance with rotational motion around a Z-Z axis.